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JPL Small-Body Database Browser
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(2014 FV32)
Classification: Apollo [NEO]          SPK-ID: 3666543
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

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For accurate long-term ephemerides, please instead use our Horizons system.This orbit viewer was implemented using two-body methods, and hence should not be used for determining accurate long-term trajectories (over several years or decades) or planetary encounter circumstances.


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Orbital Elements at Epoch 2458600.5 (2019-Apr-27.0) TDB
Reference: JPL 10 (heliocentric ecliptic J2000)
 Element Value Uncertainty (1-sigma)   Units 
e .4228587776548879 5.4511e-05  
a 1.438302660000806 9.4972e-05 au
q .8301037552950914 2.3592e-05 au
i 5.59643569545125 0.00053517 deg
node 120.9237234922426 0.00081318 deg
peri 167.6456250714233 0.00062989 deg
M 286.0624248404358 0.09971 deg
tp 2458729.900678942652
(2019-Sep-03.40067894)
0.18732 TDB
period 630.0483119553421
1.72
0.062404
0.0001709
d
yr
n .5713847544210496 5.6593e-05 deg/d
Q 2.046501564706521 0.00013513 au
  Orbit Determination Parameters
   # obs. used (total)      27  
   data-arc span      217 days  
   first obs. used      2014-03-25  
   last obs. used      2014-10-28  
   planetary ephem.      DE431  
   SB-pert. ephem.      SB431-N16  
   condition code      6  
   norm. resid. RMS      .40049  
   source      ORB  
   producer      Otto Matic  
   solution date      2017-Apr-06 08:41:57  

Additional Information
 Earth MOID = .0768877 au 
 Jupiter MOID = 3.1451 au 
 T_jup = 4.566 
[ show covariance matrix ]

Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]

Physical Parameter Table
Parameter Symbol Value Units Sigma Reference Notes
absolute magnitude H 22.6   n/a MPO294926  

[ show close-approach data ]
Ephemeris | Orbit Diagram | Orbital Elements | Mission Design | Physical Parameters | Close-Approach Data ]
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